EASA AD 2024-0086
Fuselage — Rear Fuselage — Modification
EASA Airworthiness Directive 2024-0086 is issued for Airbus A330-243 aircraft modified with EASA Supplemental Type Certificates 10064192, 10064600, or 10069256, specifically those converted to the MRTT configuration by Airbus Defence and Space S.A. This directive addresses a structural integrity issue in the rear fuselage at circumferential joint Frame 58 due to incomplete cold working during production. The AD mandates modification of the stringer couplings to ensure continued airworthiness and prevent potential catastrophic failure.